View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 58722U 26145.66668980 +.00000000 +00000-0 +27427-2 0 00008
2 58722 53.1594 232.4315 0000990 47.7017 186.1156 15.34332222 02
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0000990 |
| inclination: | 53.1594° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 232.4315° |
| argument of perigee: | 47.7017° |
| revolutions per day: | 15.34332222 |
| mean anomaly at epoch: | 186.1156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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